N206NN
Service difficulty reports · 38
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N206NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N206NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA20260825001Unknown · odorDETECTED AN ELECTRICAL BURNING SMELL IN THE FLTDECK DURING APPROACH, FAS WERE ABLE TO CONFIRM ELECTRICAL BURNING SMELL IN THE CABIN. NO EICAS MSG OR ABNORMAL SYSTEM ALARMS ACTIVATED, ALL BREAKERS IN. C/W ITEMS 1 THROUGH 8 OF TRIAD WORK SCOPE WAS UNABLE TO DUSDR SIMA20260720001Unknown · odorACRID, MUSTY ODOR PRESENT THROUGHOUT ACFT WHEN OPERATING PACKS, THE ODOR WAS MORE PREVALENT AT LOWER ALTITUDES. PER TRIAD WORK SCOPE STEP 6, PERFORM A GROUND RUN USING EACH ENGINE BLEED AIR AS A SOURCE FOR THE PACKS TO TRY DUPLICATE THE ISSUE, & ISOLATE WHICH SDR SIMA20260404003Light · unserviceableEMERGENCY PHOTOLUMINESCENT FLOOR LIGHT STRIP RH 1; 2; 3; 5; 6; 7; 8; 11 AND 12 FOUND TO BE UNSERVICEABLE COMPLETE: INSTALLED NEW APPLICABLE EMERGENCY PHOTOLUMINESCENT STRIP RH 1; 2; 3; 5; 6; 7; 8; 11 AND 12IAW AMM 33-50-21SDR SIMA20251221001Power Supply · inoperativeEMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE. TWO EMERGRENCY LIGHTS IN THE CENTER OF THE CABIN DO NOT ILLUMINATE. R & R AFT RT OTBD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. ALL LIGHTS CAME ON, NO BATT FAULT EICAS MSGSDR SIMA20250102002Control Column · obstructedYOKE IS LOCKED WILL NOT ROTATE LEFT ON FLIGHT CONTROL CHECK ONLY ROTATE RIGHT. FOUND FLASH LIGHT STUCK BETWEEN AILERON CONTROL QUADRANT ASSY AND ICC ON THE FWD AVIONICS COMPARTMENT. REMOVED FLASH LIGHT. PERF. RETURN TO SERVICE FLIGHT CONTROLS IAW AMM 27-00-00.SDR SIMA20241222001Windshield · crackedCRACK/ BUBBLE IN FO WINDSHIELD EXPANDING IN FLIGHT. EMERGENCY DECLARED. DIVERT TO ATL. OVERWEIGHT LANDING. NORMAL SINK RATE. NO INJURIES. FOUND CRACKS TO BE URETHANE INTERLAYERS EXPOSED TO MOISTURE PER AMM 56-11-00-210-801-A STEP 2.A.(6). FOUND DELAMINATION MESDR SIMA20230518001Seat Track · corrodedLH INBD SEAT TRACK BEAM IS CORRODED BY FR 18 CROSSMEMBER (LEVEL 2 CORROSION)-C/A-COMPLETE:COMPLETED REPAIR TO SEAT TRACK BEAM AT FR 18 IAW SRM 53-10-10SDR SIMA20230412005Light · crackedRH EMERGENCY LIGHT STRIPS #1,4,9 AND 11 HAVE CRACKED PLASTICS REQUIRING REPLACEMENT.-C/A-COMPLETE:INSTALLED NEW PHOTOLUMINESCENT LIGHT STRIPS IAW EMB 175 AMM 33-50-21SDR SIMA202305182004Light · crackedLH EMERGENCY LIGHT STRIPS #2,3,4,AND 7 REQUIRE REPLACEMENT DUE TO CRACKED PLASTICS.-C/A-COMPLETE:INSTALLED NEW PHOTOLUMINESCENT LIGHT STIRPS IAW EMB 175 AMM 33-50-21SDR SIMA20230323001Sensor · failedSLAT FAIL INFLIGHT. EMRGENCY DECLARED. TAXI NORMAL TO GATE. -C/A-T/S IAW FIM 27-83-00-810-810. RAR TRACK 3 INBD RH SKEW SENSOR IAW AMM 27-83-02. TAT SF-ACE 2 IAW AMM 27-53-02. OPS CHECK FAILEDSDR SIMA20210303001Eicas · activatedDOOR PAX FWD OPEN WARNING EICAS MSG DURING CLIMB FOLLOWED BY CABIN PRESSURIZATION ISSUES DECLARED EMERGENCY-C/A-CYCLED MAIN CABIN DOOR IAW SDSMM 52-11-00 ALL IND NORMAL PRESSURIZEDA/C IAW EMB AMM 21-31-00 ALL INDICATION NORMAL. NO FAULTS FOUND AT THIS TIME.SDR SIMA202007210002Unknown · odorCABIN ZONE 3 HAS CIGARETTE ODOR COMING OUT. INTERROGATED CABIN ZONE E FOR CIGARETTE ODOR IAW FIM 25-30-00-810-801-A. NO DEFECTS FOUND.SDR SIMA202006221001Light · fadedPCR EMERGENCY FLOOR STRIP INBD FWD CLOSET FADED (FOUND DURING CONFORMITY). REMOVED AND REPLACED EMERGENCY FLOOR STRIP INBD FWD CLOSET IAW AMM 33-50-21.SDR SIMA2020070204004Accumulator · lowAFT PAX DOOR SLIDE ACCUMULATOR IS LOW. REMOVED AND REPLACED AFT PAX DOOR SLIDE IAW AMM 25-65-01 TORQUMETER EASI 8238, AND TQW EASI 4327.SDR C77A2020013080011Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE FORWARD FUSELAGE RH IB SEAT TRACK (P/N 170-03263-001) BETWEEN FR13 AND FR14 IN THE FORWARD CABIN FLOOR STRUCTURE. SDR C77A2020013080010Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE FR84 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE CENTER FUSELAGE III. THE DAMAGE IS LOCATESDR C77A2020013028009Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III RH IB SEAT TRACK P/N 170-86082-005. ACCOMPLISHMENT OF THIS TRACK SPLICE REPAIR WILL BE PER ETD2020-170-001434B AND SRM 1583 PART II SDR C77A2020012980008Fire Bottle · dischargedAPU FIRE BOTTLE DISCHARGE MESSAGE DURING SYSTEM TEST. WO# 2800746437SDR C77A2020012900001Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE III RH IB SEAT TRACK P/N 170-86082-005. ACCOMPLISHMENT OF THIS TRACK SPLICE REPAIR WILL BE PER ETD2020-170-001434B AND SRM 1583 PART II SDR C77A2020012980006Gusset · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-92908-001 RH PANEL SUPPORT, P/N 170-9SDR C77A202001280054Floorbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE
DISCOVERED DURING BASIC CHECK AT EAMS ON THE UPPER FLANGE OF THE FR84 CROSSBEAM IN THE CABIN FLOOR STRUCTURE OF THE CENTER FUSELAGE III. THE DAMAGE IS LOCASDR C77A2020012800054Skin · burnedDAMAGE AREA 1, AFFECTING THE CENTER FUSELAGE I LOWER RIGHT SKIN PANEL (P/N 170-92574-005) JUST FORWARD OF FR23 AND ABOVE STGR-13R COULD NOT BE REPAIRED THROUGH A MINOR REPAIR IN ACCORDANCE WITH SRM 53-00-00/REPAIR 03P BECAUSE THE AFFECTED HOLE SIZE EXCEEDED THSDR C77A2020012800053Skin · damagedDAMAGE AREA 1, AFFECTING THE CENTER FUSELAGE I LOWER RIGHT SKIN PANEL (P/N 170-92574-005) JUST FORWARD OF FR23 AND ABOVE STGR-13R COULD NOT BE REPAIRED THROUGH A MINOR REPAIR IN ACCORDANCE WITH SRM 53-00-00/REPAIR 03P BECAUSE THE AFFECTED HOLE SIZE EXCEEDED THSDR C77A2020012800052Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE DISCOVERED DURING BASIC CHECK AT EAMS ON THE FORWARD FUSELAGE RH IB SEAT TRACK (P/N 170-03263-001) BETWEEN FR13 AND FR14 IN THE FORWARD CABIN FLOOR STRUCTURE. SDR C77A2020012800004Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-92908-001 RH PANEL SUPPORT, P/N 170-9SDR C77A2020012800003Floor Support · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-92908-001 RH PANEL SUPPORT, P/N 170-9SDR C77A2020012800002Shear Panel · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE IN THE FORWARD AND AFT CABIN FLOOR STRUCTURE BY REPLACEMENT OF THE FOLLOWING: P/N 170-05663-005 RH FLOOR SILL, P/N 170-92908-001 RH PANEL SUPPORT, P/N 170-9SDR C77A2020012800001Service Panel · corrodedWASTE SERVICING PANEL 152AR HAS CORROSION ON THE FORWARD LEFT CORNER OF THE INTERNAL SURFACE. REMOVED AND REPLACED WASTE SERVICING PANEL 152AR REF EMB AMM 20-10-02.SDR C77A2020012980007Slide · unlacedFORWARD PAX DOOR EMERGENCY EVAC SLIDE UNLACED DURING INSTALL. WO#2800746431SDR C77A2020012614077Strap · corrodedDURING BASIC CHECK AT EAMS, EAMS REPORTED CORROSION ON THE AFT STRAP FOR THE AFT BELLY FAIRING. REFER TO FIGURE 1 FOR DETAILS. COMPASS HAS DESIGNATED THIS AS A MINOR REPAIR. WORK ORDER 2818803SDR C77A2020012614076Seat Track · corrodedDURING BASIC CHECK AT EAMS, EAMS REPORTED CENTER FUSELAGE III LH INBOARD SEAT TRACK WITH CORROSION AT THE END OF THE PART. REFER TO FIGURE 1 FOR DETAILS. COMPASS ENGINEERING HAS CLASSIFIED THIS AS A MINOR REPAIR. WORK ORDER 2817744SDR C77A2020012314057Structure · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART II, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT RH WING TIP SPAR 1 (P/N 171-16231-002 OR 171-16231-004) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-171-22480-40SDR C77A2020012314056Structure · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART I, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT LH WING TIP SPAR 1 (P/N 171-16231-001 OR 171-16231-003) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-22480-401), WSDR C77A2019102800003Engine · failedENG 1 FAIL ON CLIMBOUT. LOUD BANG NOISE FOLLOWED BY LOSS OF THRUST AND ENG 1 FAIL MSG.UPON LANDING MZ PERFORMED A BORESCOPE OF AND CONFIRMED HPT BLADES MISSING. ENGINE CHANGE IN PROGRESS AS SDR SUBMITTED. SUPPLIMENTAL SDR TO FOLLOWSDR C77A2018061800001Brake Assy · failedCREW RECEIVED AN INTERMITTENT PARKING BRAKE EICAS MESSAGES DURING FLIGHT. DECLARED AN EMERGENCY. LANDED SAFELY, PARK BRAKE NOT RELEASED, QRH CLEARED ONCE, THEN MESSAGE INTERMITTENT REMAINDER OF FLIGHT, WITH BRAKE FAULT AFTER LANDING. FURTHER INSPECTION FOSDR C77A20150805004Support Fitting · dislodgedFLAP & SLAT FAIL ON RETRACTION. REMOVED RT NR 3 FLAP TRACK FAIRING IAW 57-58-25 AMM. FOUND UPPER & LOWER TRUNNION MOUNT BEARINGS DISLODGED WITH THE UPPER MIGRATED COMPLETELY OUT. LEFT NR 3 TRUNNION MOUNT, LOWER, IS ALSO DISPLACED. THIS WORK ORDER REMAINS OSDR C77A20150805003Control Lever · defectiveFLAP & SLAP FAIL AFTER TAKEOFF. PERFORMED QRH 7.10 SLAT INDICATED GREEN WITH FLAPS INDICATING AMBER & ZERO POSITION. PERFORMED FLAP PDU MOTOR BRAKE RELEASE IAW AMM 45-45-00-970-805-A/200, CONDUCTED VISUAL INSPECTION OF THE FLAP & SLAT ACTUATORS & SKEW SENSORSDR C77A20150731002Sensor · failedFLAP FAIL MESSAGE ON CLIMB OUT, 30 SECONDS AFTER FLAPS INDICATED 0. COMPLETED QRH. R & R T3 & T4 SKEW SENSORS IAW AMM 27-83-01 & 27-83-02. OPERATIONS CHECKED GOOD.
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